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Defense Intelligence Reference Document Laser Lightcraft Nanosatellites

Defense Intelligence Agency · 77 pages · text from the file's own layer

This Defense Intelligence Reference Document from the Defense Intelligence Agency, dated 1 November 2010, was produced under the Advanced Aerospace Weapon System Applications (AAWSA) Program. It describes nanosatellite technologies and proposes launching nanosats into orbit with laser Lightcraft propulsion. It also covers a weapon mission selection study and multi-megawatt laser options. The author recommends that the Department of Defense and NASA bring Lightcraft R&D back to the United States and restart the X-50LR flight demonstration program.

  • p. 3 …Laser Lightcraft Weapon Mission Selection Study .................................. 27 Chapter 4: Summary of Multi-Megawatt Laser Study for…
  • p. 5 …Many of these missions require numerous small spacecraft in a constellation or "swarm." These include orbital…
  • p. 7 …Simple, effective methods of thermal control are essential to keep the nanosat operational during extreme temperature…
  • p. 8 …GUIDANCE, NAVIGATION AND CONTROL Guidance Navigation and Control (GN&C) subsystem key technologies and concepts have…
  • p. 13 …Streamlined testing is needed for up to 100 or 1000 nanosats per mission. Performing a complete…
  • p. 14 …the mission lifetime. The remote agents achieve this goal by monitoring and appropriately controlling nanosat subsystems…
  • p. 33 …Thus, the selected Lightcraft missions are launch vehicle missions involving 29 UNCLASSIFIED//F&R 8FFI&I…
  • p. 40 …An air-launched Lightcraft launch vehicle mission, involving the transport of lasers and Lightcraft on medium…
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• Average power limited by low thermal conductivity of host material.
• Wavelengths propagate extremely well in clear weather:
- Very low absorption.
- Higher scattering.
The requirements for high average power bulk solid-state lasers are [30]:
• Efficient optical pumping of gain medium:
- Flash lamp or laser diode well matched to absorption band.
- Small wavelength difference between pump and lasing ➔ low quantum defect.
• Efficient heat removal from gain medium:
- Improved heat removal techniques from host.
- Large surface area per unit volume.
- Or, large volume to store heat with low duty cycle operation.
• Gain medium must retain good (correctable) optical quality.
The typical properties of widely used Nd :YAG lasers are [30]:
• 4 nm absorption line width.
• 24% heating from quantum loss.
• Saturation intensity:::: 3 kW/cm 2 (at:::: 2% dopant).
• Multi-kilowatt average power demonstrated.
• Maximum average power potential ~ several hundred kilowatts:
- Heat removal makes continuous running a challenge at this power.
- Current high-energy SSLs produce great amounts of heat (e.g., 600 kW of
electrical power in and 100 kW of beam power out equals 500 kW of waste
heat).
- Must store the waste heat and reject it from the system at a lower rate, thus
requiring storage and limited duty cycle.
• Quantum defect= pump light photon energy minus laser light photon energy.
The typical properties of widely used Yb:YAG lasers are [30]:
• 18 nm absorption line width.
• Indium gallium arsenide (InGaAs) pump laser diodes at 0.941 μm wavelength:
- 8.6% heating from quantum loss.
• Saturation intensity:::: 9.7 kW/cm 2 (at:::: 25% dopant).
• Multi-kilowatt average power demonstrated.
• Maximum average power potential is perhaps 5 x Nd:YAG laser.
A new technology that enables the scaling-up of BSSSL beam power is a recently
developed thermal management system that is used to remove and store the waste
heat produced by BSSSL devices. General Atomics' Advanced Power Systems Division
recently announced* that it has completed testing of an advanced thermal energy
·Reported in Space War Newsletter, June 7, 2010.
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Report, from the dia collection. The PDF is mirrored here; the original link is above. 77 pages are in the text index: search them above, or from the library's search.